Attribute | ![]() Fokker 50 × | ![]() Bombardier 415 × |
---|---|---|
General | ||
Manufacturer | Fokker | Bombardier Aerospace |
Model | Fokker 50 | Bombardier 415 |
Country | Netherlands | Canada |
Manufactured from (year) | 1987 | 1994 |
Manufactured to (year) | 1997 | 2015 |
Type | Passenger Turbo Props | Amphibious |
Icao | F50 | CL2T |
Performance | ||
Engine | 2x Pratt & Whitney PW125B turboprops | 2x 2 X Pratt & Whitney Canada PW123AF |
Power, hp (hp) | 2,500 | 2,380 |
Avionics | EFIS and Automatic Flight Control System | Honeywell EFIS, Primus II Nav/Comm Radio System |
Max cruise speed (km/h) | 530 | 359 |
Approach speed (km/h) | 180 | 126 |
Travel range (km) | 2,056 | 2,443 |
Fuel economy (km/l) | 0.44 | 0.484 |
Service ceiling (m) | 7,620 | 4,481 |
Rate of climb (m/sec) | 7.62 | 8.13 |
Take off distance (m) | 1,350 | 815 |
Landing distance (m) | 1,130 | 665 |
Weights | ||
Max take off weight (kg) | 20,820 | 19,890 |
Max landing weight (kg) | 20,030 | 16,780 |
Max payload (kg) | 5,500 | 2,903 |
Fuel tank capacity (l) | 5,137 | 5,791 |
Baggage volume (m³) | 16.72 | 1.4 |
Dimensions | ||
Seats | 62 | 18 |
Cabin height (m) | 1.96 | 1.9 |
Cabin width (m) | 2.5 | 2.4 |
Cabin length (m) | 15.63 | 9.4 |
Exterior length (m) | 25.25 | 19.8 |
Tail height (m) | 8.32 | 9 |
Fuselage diameter (m) | 2.7 | 2.69 |
Wing span (m) | 29 | 28.6 |
Wing tips | No Winglets | No Winglets |